Here's a matlab coding problem

The problem is calculate the trajectory of our cannon shell including both air drag and the reduced air density at high altitudes so that you can reproduce the results in Figure 2.5.(shown below) Perform your claculation for different firing angles and determine the value of the angle that gives the maximum range.

Another promt for the question: The output of your code should produce a well annotated plot that shows the y vs. x (trajectory) for the projectile using the isothermal model for variation in air density. Your code should also display the range of the projectile - i.e. the point where it hits the ground, when launched on a level plane.

ter 2 Realistic Projectile Motion Cannon shell trajectory 10 With density Correction Without density correction 20 x (km)